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The Laws of Motion of Artificial Satellites
Motion of the Satellite Relative to
The Rocket Starter of the Artificial Satellite
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acceleration aircraft altitude altitude of flight angle angular velocity apogee artificial satellite atmosphere axis cabin calculations carrier rocket celestial vault cent circular orbit circular velocity combustion chamber conditions of weightlessness cosmic rays decrease descent diameter direction distance earth radii earth's atmosphere earth's surface elliptical orbit energy equator equatorial exhaust velocity G-force glider gravity greater heat heavenly bodies horizontal increase instance instruments interplanetary station ionosphere kilograms kilometers per second launching an artificial length liquid lunar maximum meteoric bodies meters per second micrometeorites millimeters minutes missile moon motion necessary observer orbital rocket orbital ship oxygen perigee period of revolution poles possible pressure radiation radio waves radius relative resistance retardation revolving rocket engine rotation satel satellite flying satellite orbit sidereal day sidereal period solar rays Soviet artificial satellite space ship sphere stars synodic period Table take-off tanks temperature tion total velocity visible weight weightlessness